Evaluation of polyurethane binder additivated with paraffin and tested with a swirl injector http://arc.aiaa.org/doi/abs/10.2514/6.2012-4309
Studies on a Pressurized Swirl Injector Bi-Propellant Used in Rocket-Motor http://arc.aiaa.org/doi/abs/10.2514/6.2009-5494
Gaseous Oxygen Injection Effects in Hybrid Labscale Rocket Motor Operations http://arc.aiaa.org/doi/abs/10.2514/6.2010-6545
Combustion evaluation of PU solid fuel based on pre-polymer technology additivated with
paraffin and Aluminum for hybrid rocket engines
http://arc.aiaa.org/doi/abs/10.2514/6.2012-4008
Design and Testing of a Hybrid Rocket Motor
http://arc.aiaa.org/doi/abs/10.2514/6.2011-5755
Experimental Study of Vegetal Based Polyurethane Fuel filled with Paraffin Particles for
Hybrid Rocket Motors (AIAA 2013-4038)
http://arc.aiaa.org/doi/abs/10.2514/6.2013-4038
Thermal Decomposition Kinetics of Aged Solid Propellant Based on Ammonium Perchlorate – AP/HTPB Binder http://arc.aiaa.org/doi/abs/10.2514/6.2008-4969
Solid rocket motor burn simulation considering complex 3D propellant grain geometries (AIAA 2016-5098) http://arc.aiaa.org/doi/abs/10.2514/6.2016-5098
ITA Candy rocket motor design and solid propellant manufacture challenges (AIAA 2016-4937) http://arc.aiaa.org/doi/abs/10.2514/6.2016-4937
Detailed Study of Hydrogen Combustion in Homogeneous Reactor
http://arc.aiaa.org/doi/abs/10.2514/6.2012-4006
Benefits of Coating Applications: A Case Study
http://arc.aiaa.org/doi/abs/10.2514/6.2009-5381
Thermal Decomposition Kinetics Studies of Ammonium Perchlorate – HTPB /Al/AP Solid Propellants formulated with Iron Oxide burning rate catalyst in Nano and Micro scale (AIAA 2013-4088) http://arc.aiaa.org/doi/abs/10.2514/6.2013-4088
International Workshop on
New Energetic Materials and Propulsion / Techniques for Space Exploration
Politecnico di Milano, Campus Bovisa Sud, Room L-07 Milan, I-20156 Italy 09-10 June 2014